Problems analyzed that must be solved before titanium may be widely used, are its high cost, creep properties, fatigue strength, etc; possibility of 40% saving in deadweight indicated when using titanium alloys in crankshaft and connecting rods of reciprocating aircraft engine, in place of alloy steel. (See also Soc Automotive Engrs -- J v 60 n 8 Aug 1952 p 25-30; Iron Age v 169 n 20 May 15 1952 p 121-5; Aeroplane v 82 n 2127 Apr 25 1952 p 494-7; Aviation Week v 56 n 26 June 30 1952 p 21-2, 24-6, 29, 32)
Application of titanium to aircraft engines
Automotive Industries
Automotive Industries ; 107 , n 1
1952
Illustrations
Aufsatz (Zeitschrift)
Englisch
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Application of titanium to aircraft engines
Engineering Index Backfile | 1952
|Application of titanium to aircraft engines
Engineering Index Backfile | 1952
|Application of titanium to aircraft engines
Engineering Index Backfile | 1952
|APPLICATION OF TITANIUM TO AIRCRAFT ENGINES
SAE Technical Papers | 1952
|Application of titanium to aircraft engines
Engineering Index Backfile | 1952
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